Title :
Investigation of robust adaptive control laws for flight control system implementation
Author :
Lam, Quang M. ; Hill, Joe P.
Author_Institution :
Coleman Res. Corp., Fairfax, VA, USA
Abstract :
A direct model-following adaptive concept is used to develop control laws for helicopter flight control systems (FCSs). The robust performance of the adaptive control scheme subject to parameter variations and system nonlinearity effects is demonstrated. The scheme provides an attractive solution to FCS implementation for a modern attack helicopter with a minimal amount of software impact
Keywords :
adaptive control; aircraft control; control nonlinearities; helicopters; model reference adaptive control systems; aircraft control; direct model-following adaptive; flight control system; helicopter; robust adaptive control; system nonlinearity effects; Adaptive control; Aerospace control; Aircraft; Error correction; Helicopters; Identity-based encryption; Integral equations; Noise figure; Programmable control; Robust control;
Conference_Titel :
Control Applications, 1992., First IEEE Conference on
Conference_Location :
Dayton, OH
Print_ISBN :
0-7803-0047-5
DOI :
10.1109/CCA.1992.269780
